Your Selections

TEAAMSAM-M
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Publishers

Committees

Committee Codes

 
new

Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7008
  • Current
Published 2019-03-26 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.

 
new

Titanium Alloy, High Temperature Applications, Powder for Additive Manufacturing, Ti - 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7014
  • Current
Published 2019-03-11 by SAE International in United States

This specification covers a heat-resistant titanium alloy in the form of pre-alloyed powder.

 

Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate Ti-6Al-4V Stress Relieved

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7004
  • Current
Published 2019-01-31 by SAE International in United States
This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress relief heat treatment. This is a wire fed additive manufacturing process. If required by the CEO, preforms may require subsequent machining to meet requirements for their intended final part application.
Datasets icon
Annotation icon
 

Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7005
  • Current
Published 2019-01-31 by SAE International in United States
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
Datasets icon
Annotation icon
 

Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7013
  • Current
Published 2019-01-03 by SAE International in United States
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt.%) greater than 40 mesh (425 µm) is allowed.
Datasets icon
Annotation icon
 

Laser Powder Bed Fusion Process

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7003
  • Current
Published 2018-06-08 by SAE International in United States
This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
Datasets icon
Annotation icon
 

Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7002
  • Current
Published 2018-06-08 by SAE International in United States
This specification is to prescribe process requirements for production of metal powder feedstock for use in additive manufacturing of aerospace parts.
Datasets icon
Annotation icon
 

Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7000
  • Current
Published 2018-06-08 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition stress relief (SR), hot isostatic press (HIP) and solution anneal operations. Parts may require subsequent machining or surface finishing to meet specific application requirements.
Datasets icon
Annotation icon
 

Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7001
  • Current
Published 2018-06-08 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.
Datasets icon
Annotation icon
 

Titanium Alloy Direct Deposited Products 6Al - 4V Annealed

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS4999A
  • Current
Published 2016-09-26 by SAE International in United States
This specification covers metal products fabricated by direct metal deposition.
Datasets icon
Annotation icon